航空学报 > 1995, Vol. 16 Issue (3): 8-13

燃烧室中湍流涡旋流动的数值模拟

符松   

  1. 清华大学工程力学系,北京,100084
  • 收稿日期:1993-08-30 修回日期:1994-03-23 出版日期:1995-06-25 发布日期:1995-06-25

NUMERICAL STUDY OF COMBUSTOR TURBULENT SWIRLING FLOW

Fu Song   

  1. Department of Engineering Mechanics, Tsinghua University, Beijing, 100084
  • Received:1993-08-30 Revised:1994-03-23 Online:1995-06-25 Published:1995-06-25

摘要: ASM也进行了研究。研究的流场包括有约束的和自由的强涡旋流动。研究结果表明,二阶矩封闭模式在计算强涡旋湍流流动中很有效,代数模式则不能令人满意。计算结果可供燃烧室设计参考。

关键词: 涡动, 湍流, 燃烧室, 雷诺应力, 数值分析

Abstract: Numerical computation of turbulent strongly - swirling in combustors is presented. Turbu2lence models examined are based on the transport equations of the Reynolds stresses , i. e. , the second -moment closures. The particular flows in question include confined as well as free swirling situationswhere the swirl number is large. It is indicated that the second - moment closure models offer an effec2tive means for predicting strongly swirling flows. In particular , the Isotropization of Production and Con2vection (IPC) model gives the best overall performance. The study directly serves for the improvement ofcombustor design.

Key words: swirling, turbulence, combustor, Reynolds streeses

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